What was found
TEN BLEND-OUTS LOCATED LT FUSELAGE SKIN BETWEEN BS 1600-1640 BETWEEN S23-24L. INSTALLED DOUBLER REPAIR IAW SRM 51-40-02, ER/A 542818-14, REV 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TEN BLEND-OUTS LOCATED LT FUSELAGE SKIN BETWEEN BS 1600-1640 BETWEEN S23-24L. INSTALLED DOUBLER REPAIR IAW SRM 51-40-02, ER/A 542818-14, REV 1.